Method and device for controlled cleaving process

ABSTRACT

A technique for forming a film of material ( 12 ) from a donor substrate ( 10 ). The technique has a step of forming a stressed region in a selected manner at a selected depth ( 20 ) underneath the surface. An energy source such as pressurized fluid is directed to a selected region of the donor substrate to initiate a controlled cleaving action of the substrate ( 10 ) at the selected depth ( 20 ), whereupon the cleaving action provides an expanding cleave front to free the donor material from a remaining portion of the donor substrate.

CROSS-REFERENCES TO RELATED APPLICATIONS

This application is C.I.P. of U.S. Ser. No. 09/026,027, filed Feb. 19, 1998, now U.S. Pat. No. 5,994,207, which claims priority to U.S. Ser. No. 60/046,276, filed May 12, 1997, commonly owned and hereby incorporated by reference for all purposes.

BACKGROUND OF THE INVENTION

The present invention relates to the manufacture of substrates. More particularly, the invention provides a technique including a method and device for cleaving a substrate in the fabrication of a silicon-on-insulator substrate for semiconductor integrated circuits using a pressurized fluid, for example. But it will be recognized that the invention has a wider range of applicability; it can also be applied to other substrates for multi-layered integrated circuit devices, three-dimensional packaging of integrated semiconductor devices, photonic devices, piezoelectronic devices, microelectromechanical systems (“MEMS”), sensors, actuators, solar cells, flat panel displays (e.g., LCD, AMLCD), biological and biomedical devices, and the like.

Craftsmen or more properly crafts-people have been building useful articles, tools, or devices using less useful materials for numerous years. In some cases, articles are assembled by way of smaller elements or building blocks. Alternatively, less useful articles are separated into smaller pieces to improve their utility. A common example of these articles to be separated include substrate structures such as a glass plate, a diamond, a semiconductor substrate, and others.

These substrate structures are often cleaved or separated using a variety of techniques. In some cases, the substrates can be cleaved using a saw operation. The saw operation generally relies upon a rotating blade or tool, which cuts through the substrate material to separate the substrate material into two pieces. This technique, however, is often extremely “rough” and cannot generally be used for providing precision separations in the substrate for the manufacture of fine tools and assemblies. Additionally, the saw operation often has difficulty separating or cutting extremely hard and/or brittle materials such as diamond or glass.

Accordingly, techniques have been developed to separate these hard and/or brittle materials using cleaving approaches. In diamond cutting, for example, an intense directional thermal/mechanical impulse is directed preferentially along a crystallographic plane of a diamond material. This thermal/mechanical impulse generally causes a cleave front to propagate along major crystallographic planes, where cleaving occurs when an energy level from the thermal/mechanical impulse exceeds the fracture energy level along the chosen crystallographic plane.

In glass cutting, a scribe line using a tool is often impressed in a preferred direction on the glass material, which is generally amorphous in character. The scribe line causes a higher stress area surrounding the amorphous glass material. Mechanical force is placed on each side of the scribe line, which increases stress along the scribe line until the glass material fractures, preferably along the scribe line. This fracture completes the cleaving process of the glass, which can be used in a variety of applications including households.

Although the techniques described above are satisfactory, for the most part, as applied to cutting diamonds or household glass, they have severe limitations in the fabrication of small complex structures or precision workpieces. For instance, the above techniques are often “rough” and cannot be used with great precision in fabrication of small and delicate machine tools, electronic devices, or the like. Additionally, the above techniques may be useful for separating one large plane of glass from another, but are often ineffective for splitting off, shaving, or stripping a thin film of material from a larger substrate. Furthermore, the above techniques may often cause more than one cleave front, which join along slightly different planes, which is highly undesirable for precision cutting applications. Other processing techniques such as the use of a release layer have also had limited success. Such release layer techniques often require wet chemical etching, which is often undesirable in many state of art applications.

From the above, it is seen that a technique for separating a thin film of material from a substrate which is cost effective and efficient is often desirable.

SUMMARY OF THE INVENTION

According to the present invention, an improved technique for removing a thin film of material from a substrate using a controlled cleaving action is provided. This technique allows an initiation of a cleaving process on a substrate using a single or multiple cleave region(s) through the use of controlled energy (e.g., spatial distribution) and selected conditions to allow an initiation of a cleave front(s) and to allow it to propagate through the substrate to remove a thin film of material from the substrate.

In a specific embodiment, the present invention provides a process for forming a film of material from a donor substrate using a controlled cleaving process with a pressurized fluid. The process includes forming a stressed region in a donor substrate at a selected depth underneath a surface of the substrate, where a thickness of donor substrate material (e.g., thin film of detachable material) above the selected depth is defined. To cleave the donor substrate material, the method provides energy in the form of pressurized fluid or fluid jet to a selected region of the donor substrate to initiate a controlled cleaving action in the donor substrate, whereupon the cleaving action is made using a propagating cleave front(s) to free the donor material from a remaining portion of the donor substrate.

In an alternative embodiment, the present invention provides a process for forming a film of material from substrates. The process includes providing a bulk substrate (e.g., silicon) comprising an upper surface. The process also includes forming a first compressive layer (e.g., silicon germanium) overlying the upper surface. The process also includes forming a tensile layer (e.g., silicon germanium carbon, cleaving layer) overlying the first compressive layer. A step of forming a second compressive layer overlying the tensile layer is included. The method also includes forming a material layer (e.g., epitaxial silicon) overlying the second compressive layer. Energy is provided using a fluid to a selected region of the tensile layer to initiate and maintain a controlled cleaving action at the tensile layer, whereupon the cleaving action is made using a propagating cleave front to free the material layer from the bulk substrate.

In a further alternative embodiment, the present invention provides a process for forming a film of material from substrates. The process includes providing a bulk substrate (e.g., silicon) comprising an upper surface. The process also includes forming a cleaving layer overlying the upper surface. The process also includes forming a material layer (e.g., epitaxial silicon) overlying the cleaving layer. Energy is provided using a fluid to a selected region of the cleaving layer to initiate and maintain a controlled cleaving action at the cleaving layer, whereupon the cleaving action is made using a propagating cleave front to free the material layer from the bulk substrate. In a specific embodiment, cleaving occurs at or within the cleaving layer.

In most of the embodiments, a cleave is initiated by subjecting the material with sufficient energy to fracture the material in one region or more, causing a cleave front, without uncontrolled shattering or cracking. The cleave front formation energy (E_(c)) must often be made lower than the bulk material fracture energy (E_(mat)) at each region to avoid shattering or cracking the material. The directional energy impulse vector in diamond cutting or the scribe line in glass cutting are, for example, the means in which the cleave energy is reduced to allow the controlled creation and propagation of a cleave front. The cleave front is in itself a higher stress region and once created, its propagation requires a lower energy to further cleave the material from this initial region of fracture. The energy required to propagate the cleave front is called the cleave front propagation energy (E_(p)). The relationship can be expressed as:

E _(c) =E _(p)+[cleave front stress energy]

A controlled cleaving process is realized by reducing E_(p) along a favored direction(s) above all others and limiting the available energy to be below the E_(p) of other undesired directions. In any cleave process, a better cleave surface finish occurs when the cleave process occurs through only one expanding cleave front, although multiple cleave fronts do work.

Numerous benefits are achieved over pre-existing techniques using the present invention. In particular, the present invention uses controlled energy and selected conditions to preferentially cleave a thin film of material from a donor substrate which includes multi-material sandwiched films. This cleaving process selectively removes the thin film of material from the substrate while preventing a possibility of damage to the film or a remaining portion of the substrate. Accordingly, the remaining substrate portion can be re-used repeatedly for other applications.

Additionally, the present invention uses a relatively low temperature during the controlled cleaving process of the thin film to reduce temperature excursions of the separated film, donor substrate, or multi-material films according to other embodiments. In most cases, the controlled cleaving process can occur at, for example, room temperature, as well as others. This lower temperature approach allows for more material and process latitude such as, for example, cleaving and bonding of materials having substantially different thermal expansion coefficients. In other embodiments, the present invention limits energy or stress in the substrate to a value below a cleave initiation energy, which generally removes a possibility of creating random cleave initiation sites or fronts. This reduces cleave damage (e.g., pits, crystalline defects, breakage, cracks, steps, voids, excessive roughness) often caused in pre-existing techniques. Moreover, the present invention reduces damage caused by higher than necessary stress or pressure effects and nucleation sites caused by the energetic particles as compared to pre-existing techniques.

The present invention achieves these benefits and others in the context of known process technology. However, a further understanding of the nature and advantages of the present invention may be realized by reference to the latter portions of the specification and attached drawings.

BRIEF DESCRIPTION OF THE DRAWINGS

FIGS. 1-11 are simplified diagrams illustrating a controlled cleaving technique according to an embodiment of the present invention; and

FIGS. 12-18 are simplified cross-sectional view diagrams illustrating a method of forming a silicon-on-insulator substrate according to the present invention.

DESCRIPTION OF THE SPECIFIC EMBODIMENTS

The present invention provides a technique for removing a thin film of material from a substrate while preventing a possibility of damage to the thin material film and/or a remaining portion of the substrate. The thin film of material is attached to or can be attached to a target substrate to form, for example, a silicon-on-insulator wafer. The thin film of material can also be used for a variety of other applications. The invention will be better understood by reference to the Figs. and the descriptions below.

FIG. 1 is a simplified cross-sectional view diagram of a substrate 10 according to the present invention. The diagram is merely an illustration and should not limit the scope of the claims herein. As merely an example, substrate 10 is a silicon wafer which includes a material region 12 to be removed, which is a thin relatively uniform film derived from the substrate material. The silicon wafer 10 includes a top surface 14, a bottom surface 16, and a thickness 18. Substrate 10 also has a first side (side 1) and a second side (side 2) (which are also referenced below in the Figs.). Material region 12 also includes a thickness 20, within the thickness 18 of the silicon wafer. The present invention provides a novel technique for removing the material region 12 using the following sequence of steps.

Selected energetic particles implant 22 through the top surface 14 of the silicon wafer to a selected depth 24, which defines the thickness 20 of the material region 12, termed the thin film of material. A variety of techniques can be used to implant the energetic particles into the silicon wafer. These techniques include ion implantation using, for example, beam line ion implantation equipment manufactured from companies such as Applied Materials, Eaton Corporation, Varian, and others. Alternatively, implantation occurs using a plasma immersion ion implantation (“PIII”) technique. Examples of plasma immersion implantation techniques are described in “Recent Applications of Plasma Immersion Ion Implantation,” Paul K. Chu, Chung Chan, and Nathan W. Cheung, SEMICONDUCTOR INTERNATIONAL, pp. 165-172, June 1996, and “Plasma Immersion Ion Implantation—A Fledgling Technique for Semiconductor Processing,”, P. K. Chu, S. Qin, C. Chan, N. W. Cheung, and L. A. Larson, MATERIAL SCIENCE AND ENGINEERING REPORTS, A Review Journal, pp. 207-280, Volume R17, Nos. 6-7, (Nov. 30, 1996), which are both hereby incorporated by reference for all purposes. Furthermore, implantation can occur using ion shower. Of course, techniques used depend upon the application.

Depending upon the application, smaller mass particles are generally selected to reduce a possibility of damage to the material region 12. That is, smaller mass particles easily travel through the substrate material to the selected depth without substantially damaging the material region that the particles traverse through. For example, the smaller mass particles (or energetic particles) can be almost any charged (e.g., positive or negative) and/or neutral atoms or molecules, or electrons, or the like. In a specific embodiment, the particles can be neutral and/or charged particles including ions such as ions of hydrogen and its isotopes, rare gas ions such as helium and its isotopes, and neon. The particles can also be derived from compounds such as gases, e.g., hydrogen gas, water vapor, methane, and hydrogen compounds, and other light atomic mass particles. Alternatively, the particles can be any combination of the above particles, and/or ions and/or molecular species and/or atomic species. The particles generally have sufficient kinetic energy to penetrate through the surface to the selected depth underneath the surface.

Using hydrogen as the implanted species into the silicon wafer as an example, the implantation process is performed using a specific set of conditions. Implantation dose ranges from about 10¹⁵ to about 10¹⁸ atoms/cm², and preferably the dose is greater than about 10¹⁶ atoms/cm². Implantation energy ranges from about 1 KeV to about 1 MeV, and is generally about 50 KeV. Implantation temperature ranges from about −200 to about 600° C., and is preferably less than about 400° C. to prevent a possibility of a substantial quantity of hydrogen ions from diffusing out of the implanted silicon wafer and annealing the implanted damage and stress. The hydrogen ions can be selectively introduced into the silicon wafer to the selected depth at an accuracy of about +/−0.03 to +/−0.05 microns. Of course, the type of ion used and process conditions depend upon the application.

Effectively, the implanted particles add stress or reduce fracture energy along a region parallel to the top surface of the substrate at the selected depth. The energies depend, in part, upon the implantation species and conditions. These particles reduce a fracture energy level of the substrate at the selected depth. This allows for a controlled cleave along the implanted plane at the selected depth. Implantation can occur under conditions such that the energy state of substrate at all internal locations is insufficient to initiate a non-reversible fracture (i.e., separation or cleaving) in the substrate material. It should be noted, however, that implantation does generally cause a certain amount of defects (e.g., micro-detects) in the substrate that can be repaired by subsequent heat treatment, e.g., thermal annealing or rapid thermal annealing.

FIGS. 1A to 1C are simplified diagrams of an alternative process for forming a stressed region, which is used to cleave a film of material from a substrate. These diagrams are merely examples, which should not limit the scope of the claims herein. One of ordinary skill in the art would recognize many other variations, alternatives, and modifications. Like reference numerals are used in these diagrams as others noted here, but are not intended to be limiting. As merely an example, substrate 10 is a silicon wafer. The silicon wafer 10 includes a top surface 101 and a bottom surface 16. Substrate 10 also has a first side (side 1) and a second side (side 2). A stressed layer is formed overlying the top surface of substrate 10.

The stressed layer can be formed by a variety of techniques. The stressed layer can be formed using chemical vapor deposition, physical vapor deposition, molecular beam epitaxy (“MBE”), plating, and other techniques, which include any combination of these. The stressed layer is preferably a silicon alloy, such as silicon germanium carbon. The silicon germanium carbon layer has a stoichiometry of Si_(x)Ge_(y),C_(z) where x, y, and z are selectively adjusted during deposition. Adjustment can occur by changing flow rates of respective mass flow controllers. The ratio of silicon to germanium to carbon is selectively adjusted to provide a desired cleaving action according to the present invention. The stressed layer can also be an epitaxial silicon layer. The epitaxial silicon layer is made using an epitaxial reactor. An example of such a reactor is an epi-Centura™ reactor made by Applied Materials, Inc. of Santa Clara, Calif. Other reactors such as those made by ASM and other companies can also be used. Other materials can also be used.

Preferably, the stressed layer is a multiple layered structure 103A according to an embodiment of the present invention. The multiple or multilayered structure 103A includes a first compressional layer 303, an overlying layer 301 under tensile stress, an overlying second compressional layer 305. The compressional layer or layers can be a silicon germanium layer or other layer. For example, the silicon germanium layer has a stoichiometry of Si_(x)Ge_(y), where x=0.9 and y=0.1. The ratio between x and y are selectively adjusted during deposition to achieve a desired result. The tensile layer can be a silicon germanium carbon layer or the like Alternatively, the tensile layer can be a silicon layer that is a heavily doped P++ layer (e.g., boron doped, in-situ boron doped) or the like. The present multiple layered structure can be formed by distinct layers or graded layers, depending upon the application. In other embodiments, each of these layers can also be doped using in-situ deposition techniques and/or implantation techniques. Implantation can include introducing impurities such as hydrogen, helium, nitrogen, boron, and other species, which selectively provides a tensile or compressive characteristic to the layer. Other techniques such as diffusion of impurities can also be used to introduce impurities into any one of the layers.

Overlying the stressed layer is a material layer 105, which can be formed by a variety of techniques. In a specific embodiment, the material layer is a layer where the device or devices are formed thereon. The material layer is a high quality layer of silicon for example. The material layer can be deposited using chemical vapor deposition, MBE, physical vapor deposition, plating, and other techniques, which include any combination of these. In a preferred embodiment, the material layer is a crystalline silicon layer or epitaxial silicon layer. The epitaxial silicon layer is made by depositing epitaxial silicon that may be doped using one or more dopants. These dopants include among others, boron, phosphorous, arsenic, and oxygen or any combination thereof. The material layer has an upper surface 14, which is the same reference number noted above.

After forming the stressed layer and the overlying material layer, a desired amount of stress is achieved. The stress can be tensile or compressive. As shown, stressed layer 103 is tensile 107 or compressive 109. Although the above has been described in terms of a single stressed layer, multiple stressed layers can be used. Alternatively, stressed layers can be combined with other layers. Additionally, a single material layer has been described. The single material layer can be replaced by multiple material layers and the like. Each of these layers can be homogeneous or graded or non-homogeneous or any combinations thereof. In the following discussion, the material layer is removed or cleaved from the stressed layer using a controlled cleaving action. The material layer can also be formed using an in-situ doping process, which can be homogeneous or graded, depending upon the application. Other ways of forming a stressed layer are described below.

FIGS. 1E to 1F are simplified diagrams of an alternative process for forming a stressed region, which is used to cleave a film of material from a substrate. These diagrams are merely examples, which should not limit the scope of the claims herein. One of ordinary skill in the art would recognize many other variations, alternatives, and modifications. Like reference numerals are used in these diagrams as others noted here, but are not intended to be limiting. Substrate 10 is a silicon wafer which includes a material region 12 to be removed, which is a thin relatively uniform film derived from the substrate material. The silicon wafer 10 includes a top surface 14, a bottom surface 16, and a thickness 18. Substrate 10 also has a first side (side 1) and a second side (side 2) (which are also referenced below in the FIGS.). Material region 12 also includes a thickness 20, within the thickness 18 of the silicon wafer. The present invention provides a novel technique for removing the material region 12 using the following sequence of steps.

Selected energetic particles implant 111 through the top surface 14 of the silicon wafer to a region 111A underlying a selected depth 24, which defines the thickness 20 of the material region 12, termed the thin film of material. A variety of techniques can be used to implant the energetic particles into the silicon wafer. These techniques include ion implantation using, for example, beam line ion implantation equipment manufactured from companies such as Applied Materials, Eaton Corporation, Varian, and others. Alternatively, implantation occurs using a plasma immersion ion implantation (“PIII”) technique. Examples of plasma immersion implantation techniques are described in “Recent Applications of Plasma Immersion Ion Implantation,” Paul K. Chu, Chung Chan, and Nathan W. Cheung, SEMICONDUCTOR INTERNATIONAL, pp. 165-172, June 1996, and “Plasma Immersion Ion Implantation—A Fledgling Technique for Semiconductor Processing,”, P. K. Chu, S. Qin, C. Chan, N. W. Cheung, and L. A. Larson, MATERIAL SCIENCE AND ENGINEERING REPORTS, A Review Journal, pp. 207-280, Volume R17, Nos. 6-7, (Nov. 30, 1996), which are both hereby incorporated by reference for all purposes. Furthermore, implantation can occur using ion shower. Of course, techniques used depend upon the application.

Selected energetic particles 113 particles implant 111 through the top surface 14 of the silicon wafer to a region 113A overlying a selected depth 24, which defines the thickness 20 of the material region 12, termed the thin film of material. A variety of techniques can be used to implant the energetic particles into the silicon wafer. These techniques include ion implantation using, for example, beam line ion implantation equipment manufactured from companies such as Applied Materials, Eaton Corporation, Varian, and others. Alternatively, implantation occurs using a plasma immersion ion implantation (“PIII”) technique. Examples of plasma immersion implantation techniques were noted. Furthermore, implantation can occur using ion shower. Of course, techniques used depend upon the application.

Depending upon the application, particles that increase a strength of the regions 111A, 113A can be used. These particles can be almost any charged (e.g., positive or negative) and/or neutral atoms or molecules, or the like. In a specific embodiment, the particles can be neutral and/or charged particles including ions such as ions of nitrogen or oxygen. The particles can also be derived from compounds such as gases. Alternatively, the particles can be any combination of the above particles, and/or ions and/or molecular species and/or atomic species. The particles generally have sufficient kinetic energy to penetrate through the surface to the selected depth underneath the surface.

Effectively, the implanted particles add stress or reduce fracture energy along a region parallel to the top surface of the substrate at the selected depth. The energies depend, in part, upon the implantation species and conditions. These particles reduce a fracture energy level of the substrate at the selected depth. This allows for a controlled cleave along the implanted plane at the selected depth. Implantation can occur under conditions such that the energy state of substrate at all internal locations is insufficient to initiate a non-reversible fracture (i.e., separation or cleaving) in the substrate material. It should be noted, however, that implantation does generally cause a certain amount of defects (e.g., micro-detects) in the substrate that can be repaired by subsequent heat treatment, e.g., thermal annealing or rapid thermal annealing. As merely an example, FIG. 1F is a diagram 120 that represents strength 121 against depth 123 along a depth of the substrate. The diagram shows an increased strength on each side of the selective depth (z_(o)). As shown, the strength at the selected depth is lower than adjacent material regions 111A, 113A. The selected depth also is a stressed region. The stressed region is cleaved according to the techniques described herein.

FIG. 1G is a simplified diagram of stress for a multilayered cleaving region according to an embodiment of the present invention. Such multilayered cleaving region is shown, for example, in FIG. 1C. Before cleaving, the multilayered structure includes a tensile region 127, which is sandwiched between compressed regions 125, 129. In a specific embodiment, the tensile region guides the controlled cleaving processes, which is bounded by the compressed regions. This multilayered region allows for preferential cleaving along the tensile region, which does not substantially damage a material or device region. Details of the cleaving action are noted below.

FIG. 2 is a simplified energy diagram 200 along a cross-section of the stressed substrate according to the present invention. The diagram is merely an illustration and should not limit the scope of the claims herein. The simplified diagram includes a vertical axis 201 that represents an energy level (E) (or additional energy) to cause a cleave in the substrate. A horizontal axis 203 represents a depth or distance from the bottom of the wafer to the top of the wafer. After introducing stress (e.g., implant, chemical vapor deposition) into the wafer, the substrate has an average cleave energy represented as E 205, which is the amount of energy needed to cleave the wafer along various cross-sectional regions along the wafer depth. The cleave energy (E_(c)) is equal to the bulk material fracture energy (E_(mat)) in non-implanted regions, for example. At the selected depth 20, energy (E_(cz)) 207 is lower since implanted particles essentially break or weaken bonds in the crystalline structure (or increase stress caused by a presence of particles or differing materials also contributing to lower energy (E_(cz)) 207 of the substrate) to lower the amount of energy needed to cleave the substrate at the selected depth. Using a CVD deposited film with differing stoichiometry, stress in the selected region can be tailored or modified in a desirable manner through lattice mismatched thin film. The strained layer can effectively reduce the selected regions fracture energy. The present invention takes advantage of the lower energy (or increased stress) at the selected depth to cleave the thin film in a controlled manner.

Substrates, however, are not generally free from defects or “weak” regions across the possible cleave front or selected depth z_(o) after the implantation process. In these cases, the cleave generally cannot be controlled, since they are subject to random variations such as bulk material non-uniformities, built-in stresses, defects, and the like. FIG. 3 is a simplified energy diagram 300 across a cleave front for the stressed substrate 10 having these defects. The diagram 300 is merely an illustration and should not limit the scope of the claims herein. The diagram has a vertical axis 301 which represents additional energy (E) and a horizontal axis 303 which represents a distance from side 1 to side 2 of the substrate, that is, the horizontal axis represents regions along the cleave front of the substrate. As shown, the cleave front has two regions 305 and 307 represented as region 1 and region 2, respectively, which have cleave energies less than the average cleave energy (E_(cz)) 207 (possibly due to a higher concentration of defects or the like). Accordingly, it is highly likely that the cleave process begins at one or both of the above regions, since each region has a lower cleave energy than surrounding regions.

An example of a cleave process for the substrate illustrated by the above Fig. is described as follows with reference to FIG. 4. FIG. 4 is a simplified top-view diagram 400 of multiple cleave fronts 401, 403 propagating through the stressed substrate. The cleave fronts originate at “weaker” regions in the cleave plane, which specifically includes regions 1 and 2. The cleave fronts originate and propagate randomly as shown by the arrows. A limitation with the use of random propagation among multiple cleave fronts is the possibility of having different cleave fronts join along slightly different planes or the possibility of forming cracks, which is described in more detail below.

FIG. 5 is a simplified cross-sectional view 500 of a film cleaved from a wafer having multiple cleave fronts at, for example, regions 1 305 and 2 307. This diagram is merely an illustration and should not limit the scope of the claims herein. As shown, the cleave from region 1 joined with the cleave from region 2 at region 3 309, which is defined along slightly different planes, may initiate a secondary cleave or crack 311 along the film. Depending upon the magnitude of the difference 313, the film may not be of sufficient quality for use in manufacture of substrates for integrated circuits or other applications. A substrate having crack 311 generally cannot be used for processing. Accordingly, it is generally undesirable to cleave a wafer using multiple fronts in a random manner. An example of a technique which may form multiple cleave fronts in a random manner is described in U.S. Pat. No. 5,374,564, which is in the name of Michel Bruel (“Bruel”), and assigned to Commissariat A l'Energie Atomique in France. Bruel generally describes a technique for cleaving a stressed wafer by global thermal treatment (i.e., thermally treating the entire plane of the implant) using thermally activated diffusion. Global thermal treatment of the substrate generally causes an initiation of multiple cleave fronts which propagate independently. In general, Bruel discloses a technique for an “uncontrollable” cleaving action by way of initiating and maintaining a cleaving action by a global thermal source, which may produce undesirable results. These undesirable results include potential problems such as an imperfect joining of cleave fronts, an excessively rough surface finish on the surface of the cleaved material since the energy level for maintaining the cleave exceeds the amount required, and many others. The present invention overcomes the formation of random cleave fronts by a controlled distribution or selective positioning of energy on the stressed substrate.

FIG. 6 is a simplified cross-sectional view of substrate 10 using selective positioning of cleave energy according to the present invention. This diagram is merely an illustration, and should not limit the scope of the claims herein. The stressed (e.g., implanted) wafer undergoes a step of selective energy placement 601 or positioning or targeting which provides a controlled cleaving action of the material region 12 at the selected depth 603. In preferred embodiments, selected energy placement 607 occurs near an edge or corner region of the selected depth 603 of substrate 10. The impulse (or impulses) is provided using energy sources. Examples of sources include, among others, a chemical source, a mechanical source, an electrical source, and a thermal sink or source. The chemical source can include a variety such as particles, fluids, gases, or liquids. These chemical sources can also include chemical reaction to increase stress in the material region. The chemical source is introduced as flood, time-varying, spatially varying, or continuous. In other embodiments, a mechanical source is derived from rotational, translational, compressional, expansional, or ultrasonic energies. The mechanical source can be introduced as flood, time-varying, spatially varying, or continuous. In further embodiments, the electrical source is selected from an applied voltage or an applied electromagnetic field, which is introduced as flood, time-varying, spatially varying, or continuous. In still further embodiments, the thermal source or sink is selected from radiation, convection, or conduction. This thermal source can be selected from, among others, a photon beam, a fluid jet, a liquid jet, a gas jet, an electro/magnetic field, an electron beam, a thermo-electric heating, a furnace, and the like. The thermal sink can be selected from a fluid jet, a liquid jet, a gas jet, a cryogenic fluid, a super-cooled liquid, a thermoelectric cooling means, an electro/magnetic field, and others. Similar to the previous embodiments, the thermal source is applied as flood, time-varying, spatially varying, or continuous. Still further, any of the above embodiments can be combined or even separated, depending upon the application. Of course, the type of source used depends upon the application.

FIG. 6 is a simplified cross-sectional view of a stressed (e.g., implanted, layered) substrate 10 using selective positioning of cleave energy according to the present invention. This diagram is merely an illustration, and should not limit the scope of the claims herein. The wafer undergoes a step of selective energy placement 601 or positioning or targeting which provides a controlled cleaving action of the material region 12 at the selected depth 603. In preferred embodiments, selected energy placement 607 occurs near an edge or corner region of the selected depth 603 of substrate 10. The impulse (or impulses) is provided using energy sources. Examples of sources include, among others, a chemical source, a mechanical source, an electrical source, and a thermal sink or source. The chemical source can include a variety such as particles, fluids, gases, or liquids. These chemical sources can also include chemical reaction to increase stress in the material region. The chemical source is introduced as flood, time-varying, spatially varying, or continuous. In other embodiments, a mechanical source is derived from rotational, translational, compressional, expansional, or ultrasonic energies. The mechanical source can be introduced as flood, time-varying, spatially varying, or continuous. In further embodiments, the electrical source is selected from an applied voltage or an applied electromagnetic field, which is introduced as flood, time-varying, spatially varying, or continuous. In still further embodiments, the thermal source or sink is selected from radiation, convection, or conduction. This thermal source can be selected from, among others, a photon beam, a fluid jet, a liquid jet, a gas jet, an electro/magnetic field, an electron beam, a thermo-electric heating, a furnace, and the like. The thermal sink can be selected from a fluid jet, a liquid jet, a gas jet, a cryogenic fluid, a super-cooled liquid, a thermo-electric cooling means, an electro/magnetic field, and others. Similar to the previous embodiments, the thermal source is applied as flood, time-varying, spatially varying, or continuous. Still further, any of the above embodiments can be combined or even separated, depending upon the application. Of course, the type of source used depends upon the application.

In a specific embodiment, the energy source can be a fluid jet that is pressurized (e.g., compressional) according to an embodiment of the present invention. FIG. 6A shows a simplified cross-sectional view diagram of a fluid jet from a fluid nozzle 608 used to perform the controlled cleaving process according to an embodiment of the present invention. The fluid jet 607 (or liquid jet or gas jet) impinges on an edge region of substrate 10 to initiate the controlled cleaving process. The fluid jet from a compressed or pressurized fluid source is directed to a region at the selected depth 603 to cleave a thickness of material region 12 from substrate 10 using force, e.g., mechanical, chemical, thermal. As shown, the fluid jet separates substrate 10 into two regions, including region 609 and region 611 that separate from each other at selected depth 603. The fluid jet can also be adjusted to initiate and maintain the controlled cleaving process to separate material 12 from substrate 10. Depending upon the application, the fluid jet can be adjusted in direction, location, and magnitude to achieve the desired controlled cleaving process. The fluid jet can be a liquid jet or a gas jet or a combination of liquid and gas.

In a preferred embodiment, the energy source can be a compressional source such as, for example, compressed fluid that is static. FIG. 6B shows a simplified cross-sectional view diagram of a compressed fluid source 607 according to an embodiment of the present invention. The compressed fluid source 607 (e.g., pressurized liquid, pressurized gas) is applied to a sealed chamber 621, which surrounds a periphery or edge of the substrate 10. As shown, the chamber is enclosed by device 623, which is sealed by, for example, o-rings 625 or the like, and which surrounds the outer edge of the substrate. The chamber has a pressure maintained at P_(C) that is applied to the edge region of substrate 10 to initiate the controlled cleaving process at the selected depth of stressed material. The outer surface or face of the substrate is maintained at pressure P_(A) which can be ambient pressure e.g., 1 atmosphere or less. A pressure differential exists between the pressure in the chamber, which is higher, and the ambient pressure. The pressure difference applies force to the stressed region at the selected depth 603. The stressed region at the selected depth can be structurally weaker than surrounding regions, including any bonded regions. Force is applied via the pressure differential until the controlled cleaving process is initiated. The controlled cleaving process separates the thickness of material 609 from substrate material 611 to split the thickness of material from the substrate material at the selected depth. Additionally, pressure P_(C) forces material region 12 to separate by a “prying action” from substrate material 611. During the cleaving process, the pressure in the chamber can also be adjusted to initiate and maintain the controlled cleaving process to separate material 12 from substrate 10. Depending upon the application, the pressure can be adjusted in magnitude to achieve the desired controlled cleaving process. The fluid pressure can be derived from a liquid or a gas or a combination of liquid and gas.

Optionally, the present cleaving technique uses a cleave initiation technique. In some embodiments, the present cleaving technique initiates at a physical region where the fluid jet is directed. Alternatively, the present cleaving technique initiates using a chemical etchant or the like, which is applied to a region where the fluid jet is to be directed. Such chemical etchant selectively weakens this region to help initiate the cleaving action. Alternatively, a mechanical member is used to physically initiate the cleaving action. The mechanical member can cause a blunt indent in the selected material region to cause a Hertzian cone crack. Still further, an implanting method can be used to localize a weak region, which will initiate the cleaving action. Moreover, a thermal means such as a laser source can be used. Other techniques can also be used to initiate the cleaving action.

In a specific embodiment, the present invention provides a controlled-propagating cleave. The controlled-propagating cleave uses multiple successive impulses to initiate and perhaps propagate a cleaving process 700, as illustrated by FIG. 7. This diagram is merely an illustration, and should not limit the scope of the claims herein. As shown, the impulse is directed at an edge of the substrate, which propagates a cleave front toward the center of the substrate to remove the material layer from the substrate. In this embodiment, a source applies multiple pulses (i.e., pulse 1, 2, and 3) successively to the substrate. Pulse 1 701 is directed to an edge 703 of the substrate to initiate the cleave action. Pulse 2 705 is also directed at the edge 707 on one side of pulse 1 to expand the cleave front. Pulse 3 709 is directed to an opposite edge 711 of pulse 1 along the expanding cleave front to further remove the material layer from the substrate. The combination of these impulses or pulses provides a controlled cleaving action 713 of the material layer from the substrate.

FIG. 8 is a simplified illustration of selected energies 800 from the pulses in the preceding embodiment for the controlled-propagating cleave. This diagram is merely an illustration, and should not limit the scope of the claims herein. As shown, the pulse 1 has an energy level which exceeds average cleaving energy (E), which is the necessary energy for initiating the cleaving action. Pulses 2 and 3 are made using lower energy levels along the cleave front to maintain or sustain the cleaving action. In a specific embodiment, the pulse is a laser pulse where an impinging beam heats a selected region of the substrate through a pulse and a thermal pulse gradient causes supplemental stresses which together exceed cleave formation or propagation energies, which create a single cleave front. In preferred embodiments, the impinging beam heats and causes a thermal pulse gradient simultaneously, which exceed cleave energy formation or propagation energies. More preferably, the impinging beam cools and causes a thermal pulse gradient simultaneously, which exceed cleave energy formation or propagation energies.

Optionally, a built-in energy state of the substrate or stress can be globally raised toward the energy level necessary to initiate the cleaving action, but not enough to initiate the cleaving action before directing the multiple successive impulses to the substrate according to the present invention. The global energy state of the substrate can be raised or lowered using a variety of sources such as chemical, mechanical, thermal (sink or source), or electrical, alone or in combination. The chemical source can include a variety such as particles, fluids, gases, or liquids. These sources can also include chemical reaction to increase stress in the material region. The chemical source is introduced as flood, time-varying, spatially varying, or continuous. In other embodiments, a mechanical source is derived from rotational, translational, compressional, expansional, or ultrasonic energies. The mechanical source can be introduced as flood, time-varying, spatially varying, or continuous. In further embodiments, the electrical source is selected from an applied voltage or an applied electromagnetic field, which is introduced as flood, time-varying, spatially varying, or continuous. In still further embodiments, the thermal source or sink is selected from radiation, convection, or conduction. This thermal source can be selected from, among others, a photon beam, a fluid jet, a liquid jet, a gas jet, an electro/magnetic field, an electron beam, a thermo-electric heating, and a furnace. The thermal sink can be selected from a fluid jet, a liquid jet, a gas jet, a cryogenic fluid, a super-cooled liquid, a thermo-electric cooling means, an electro/magnetic field, and others. Similar to the previous embodiments, the thermal source is applied as flood, time-varying, spatially varying, or continuous. Still further, any of the above embodiments can be combined or even separated, depending upon the application. Of course, the type of source used also depends upon the application. As noted, the global source increases a level of energy or stress in the material region without initiating a cleaving action in the material region before providing energy to initiate the controlled cleaving action.

In a specific embodiment, an energy source elevates an energy level of the substrate cleave plane above its cleave front propagation energy but is insufficient to cause self-initiation of a cleave front. In particular, a thermal energy source or sink in the form of heat or lack of heat (e.g., cooling source) can be applied globally to the substrate to increase the energy state or stress level of the substrate without initiating a cleave front. Alternatively, the energy source can be electrical, chemical, or mechanical. A directed energy source provides an application of energy to a selected region of the substrate material to initiate a cleave front which self-propagates through the stressed region of the substrate until the thin film of material is removed. A variety of techniques can be used to initiate the cleave action. These techniques are described by way of the Figs. below.

FIG. 9 is a simplified illustration of an energy state 900 for a controlled cleaving action using a single controlled source according to an aspect of the present invention. This diagram is merely an illustration, and should not limit the scope of the claims herein. In this embodiment, the energy level or state of the substrate is raised using a global energy source above the cleave front propagation energy state, but is lower than the energy state necessary to initiate the cleave front. To initiate the cleave front, an energy source such as a laser directs a beam in the form of a pulse at an edge of the substrate to initiate the cleaving action. Alternatively, the energy source can be a cooling fluid (e.g., liquid, gas) that directs a cooling medium in the form of a pulse at an edge of the substrate to initiate the cleaving action. The global energy source maintains the cleaving action which generally requires a lower energy level than the initiation energy.

An alternative aspect of the invention is illustrated by FIGS. 10 and 11. FIG. 10 is a simplified illustration of a stressed substrate 1000 undergoing rotational forces 1001, 1003. This diagram is merely an illustration, and should not limit the scope of the claims herein. As shown, the substrate includes a top surface 1005, a bottom surface 1007, and an stressed region 1009 at a selected depth. An energy source increases a global energy level of the substrate using a light beam or heat source to a level above the cleave front propagation energy state, but lower than the energy state necessary to initiate the cleave front. The substrate undergoes a rotational force turning clockwise 1001 on top surface and a rotational force turning counter-clockwise 1003 on the bottom surface which creates stress at the stressed region 1009 to initiate a cleave front. Alternatively, the top surface undergoes a counter-clockwise rotational force and the bottom surface undergoes a clockwise rotational force. Of course, the direction of the force generally does not matter in this embodiment.

FIG. 11 is a simplified diagram of an energy state 1100 for the controlled cleaving action using the rotational force according to the present invention. This diagram is merely an illustration, and should not limit the scope of the claims herein. As previously noted, the energy level or state of the substrate is raised using a global energy source (e.g., thermal, beam) above the cleave front propagation energy state, but is lower than the energy state necessary to initiate the cleave front. To initiate the cleave front, a mechanical energy means such as rotational force applied to the stressed region initiates the cleave front. In particular, rotational force applied to the stressed region of the substrates creates zero stress at the center of the substrate and greatest at the periphery, essentially being proportional to the radius. In this example, the central initiating pulse causes a radially expanding cleave front to cleave the substrate.

The removed material region provides a thin film of silicon material for processing. The silicon material possesses limited surface roughness and desired planarity characteristics for use in a silicon-on-insulator substrate. In certain embodiments, the surface roughness of the detached film has features that are less than about 60 nm, or less than about 40 nm, or less than about 20 nm. Accordingly, the present invention provides thin silicon films which can be smoother and more uniform than pre-existing techniques.

In a preferred embodiment, the present invention is practiced at temperatures that are lower than those used by pre-existing techniques. In particular, the present invention does not require increasing the entire substrate temperature to initiate and sustain the cleaving action as pre-existing techniques. In some embodiments for silicon wafers and hydrogen implants, substrate temperature does not exceed about 400° C. during the cleaving process. Alternatively, substrate temperature does not exceed about 350° C. during the cleaving process. Alternatively, substrate temperature is kept substantially below implanting temperatures via a thermal sink, e.g., cooling fluid, cryogenic fluid. Accordingly, the present invention reduces a possibility of unnecessary damage from an excessive release of energy from random cleave fronts, which generally improves surface quality of a detached film(s) and/or the substrate(s). Accordingly, the present invention provides resulting films on substrates at higher overall yields and quality.

The above embodiments are described in terms of cleaving a thin film of material from a substrate. The substrate, however, can be disposed on a workpiece such as a stiffener or the like before the controlled cleaving process. The workpiece joins to a top surface or implanted surface of the substrate to provide structural support to the thin film of material during controlled cleaving processes. The workpiece can be joined to the substrate using a variety of bonding or joining techniques, e.g., electro-statics, adhesives, interatomic. Some of these bonding techniques are described herein. The workpiece can be made of a dielectric material (e.g., quartz, glass, sapphire, silicon nitride, silicon dioxide), a conductive material (silicon, silicon carbide, polysilicon, group III/V materials, metal), and plastics (e.g., polyimide-based materials). Of course, the type of workpiece used will depend upon the application.

Alternatively, the substrate having the film to be detached can be temporarily disposed on a transfer substrate such as a stiffener or the like before the controlled cleaving process. The transfer substrate joins to a top surface or implanted surface of the substrate having the film to provide structural support to the thin film of material during controlled cleaving processes. The transfer substrate can be temporarily joined to the substrate having the film using a variety of bonding or joining techniques, e.g., electro-statics, adhesives, interatomic. Some of these bonding techniques are described herein. The transfer substrate can be made of a dielectric material (e.g., quartz, glass, sapphire, silicon nitride, silicon dioxide), a conductive material (silicon, silicon carbide, polysilicon, group III/V materials, metal), and plastics (e.g., polyimide-based materials). Of course, the type of transfer substrate used will depend upon the application. Additionally, the transfer substrate can be used to remove the thin film of material from the cleaved substrate after the controlled cleaving process.

A process for fabricating a silicon-on-insulator substrate according to the present invention may be briefly outlined as follows:

(1) Provide a donor silicon wafer (which may be coated with a dielectric material);

(2) Form stressed region in the donor silicon wafer at a selected depth to define a thickness of silicon film;

(3) Form device layer or material layer overlying the stressed layer (optional);

(4) Provide a target substrate material (which may be coated with a dielectric material);

(5) Bond the donor silicon wafer to the target substrate material by joining the face to the target substrate material;

(6) Increase global stress (or energy) of stressed region at selected depth without initiating a cleaving action (optional);

(7) Provide stress (or energy) using a fluid jet to a selected region of the bonded substrates to initiate a controlled cleaving action at the selected depth;

(8) Provide additional energy to the bonded substrates to sustain the controlled cleaving action to free the thickness of silicon film from the silicon wafer (optional);

(9) Complete bonding of donor silicon wafer to the target substrate; and

(10) Polish and/or smooth a surface of the thickness of silicon film.

The above sequence of steps provides a step of initiating a controlled cleaving action using an energy applied to a selected region(s) of a multi-layered substrate structure to form a cleave front(s) according to the present invention. This initiation step begins a cleaving process in a controlled manner by limiting the amount of energy applied to the substrate. Further propagation of the cleaving action can occur by providing additional energy to selected regions of the substrate to sustain the cleaving action, or using the energy from the initiation step to provide for further propagation of the cleaving action. This sequence of steps is merely an example and should not limit the scope of the claims defined herein. Further details with regard to the above sequence of steps are described in below in references to the Figs.

FIGS. 12-18 are simplified cross-sectional view diagrams of substrates undergoing a fabrication process for a silicon-on-insulator wafer according to the present invention. The process begins by providing a semiconductor substrate similar to the silicon wafer 2100, as shown by FIG. 12. Substrate or donor includes a material region 2101 to be removed, which is a thin relatively uniform film derived from the substrate material. The silicon wafer includes a top surface 2103, a bottom surface 2105, and a thickness 2107. Material region also includes a thickness (z₀), within the thickness 2107 of the silicon wafer. Optionally, a dielectric layer 2102 (e.g., silicon nitride, silicon oxide, silicon oxynitride) overlies the top surface of the substrate. The present process provides a novel technique for removing the material region 2101 using the following sequence of steps for the fabrication of a silicon-on-insulator wafer.

Selected energetic particles 2109 implant through the top surface of the silicon wafer to a selected depth, which defines the thickness of the material region, termed the thin film of material. As shown, the particles have a desired concentration 2111 at the selected depth (z₀). A variety of techniques can be used to implant the energetic particles into the silicon wafer. These techniques include ion implantation using, for example, beam line ion implantation equipment manufactured from companies such as Applied Materials, Eaton Corporation, Varian, and others. Alternatively, implantation occurs using a plasma immersion ion implantation (“PIII”) technique. Furthermore, implantation can occur using ion shower. Of course, techniques used depend upon the application.

Depending upon the application, smaller mass particles are generally selected to reduce a possibility of damage to the material region. That is, smaller mass particles easily travel through the substrate material to the selected depth without substantially damaging the material region that the particles traversed through. For example, the smaller mass particles (or energetic particles) can be almost any charged (e.g., positive or negative) and/or neutral atoms or molecules, or electrons, or the like. In a specific embodiment, the particles can be neutral and/or charged particles including ions of hydrogen and its isotopes, rare gas ions such as helium and its isotopes, and neon. The particles can also be derived from compounds such as gases, e.g., hydrogen gas, water vapor, methane, and other hydrogen compounds, and other light atomic mass particles. Alternatively, the particles can be any combination of the above particles, and/or ions and/or molecular species and/or atomic species.

There are other ways of forming a stressed region 2111 in the silicon wafer. Some of these techniques were noted above. For example, FIG. 12A is a simplified diagram of an alternative process for forming a stressed region, which is used to cleave a film of material from a substrate. This diagram is merely an example, which should not limit the scope of the claims herein. One of ordinary skill in the art would recognize many other variations, alternatives, and modifications. As merely an example, substrate 3010 is a silicon wafer. The silicon wafer 3010 includes a top surface 3101 and a bottom surface 3016. Substrate 3010 also has a first side (side 1) and a second side (side 2). A stressed layer 3103 is formed overlying the top surface of substrate 3010.

The stressed layer can be formed by a variety of techniques. The stressed layer can be formed using chemical vapor deposition, physical vapor deposition, molecular beam epitaxy (“MBE”), plating, and other techniques, which include any combination of these. The stressed layer is preferably a silicon alloy, such as silicon germanium carbon. The silicon germanium carbon layer has a stoichiometry of Si_(x)Ge_(y),C_(z) where x, y, and z are selectively adjusted during deposition. Adjustment can occur by changing flow rates of respective mass flow controllers. The ratio of silicon to germanium to carbon is selectively adjusted to provide a desired cleaving action according to the present invention. The stressed layer can also be an epitaxial silicon layer. The epitaxial silicon layer is made using an epitaxial reactor. An example of such a reactor is an epi-Centura™ reactor made by Applied Materials, Inc. of Santa Clara, Calif. Other reactors such as those made by ASM and other companies can also be used. Other materials can also be used.

Preferably, the stressed layer is a multiple layered structure according to an embodiment of the present invention. The multiple or multilayered structure includes a first compressional layer, an overlying layer under tensile stress, an overlying second compressional layer. The compressional layer or layers can be a silicon germanium layer or other layer. For example, the silicon germanium layer has a stoichiometry of Si_(x)Ge_(y), where x=0.9 and y=0.1. The ratio between x and y are selectively adjusted during deposition to achieve a desired result. The tensile layer can be a silicon germanium carbon layer or the like. Alternatively, the tensile layer can be a silicon layer that is a heavily doped P⁺⁺ layer (e.g., boron doped, in-situ boron doped) or the like. The present multiple layered structure can be formed by distinct layers or graded layers, depending upon the application.

Overlying the stressed layer is a material layer 3105, which can be formed by a variety of techniques. In a specific embodiment, the material layer is a layer where the device or devices are formed thereon. The material layer is a high quality layer of silicon for example. The material layer can be deposited using chemical vapor deposition, MBE, physical vapor deposition, plating, and other techniques, which include any combination of these. In a preferred embodiment, the material layer is a crystalline silicon layer or epitaxial silicon layer. The epitaxial silicon layer is made by depositing epitaxial silicon that is doped using one or more dopants. These dopants include among others, boron, phosphorous, arsenic, oxygen, or any combination thereof. The material layer has an upper surface 3014, which is the same reference number noted above.

After forming the stressed layer and the overlying material layer, a desired amount of stress is achieved. The stress can be tensile or compressive or any combination thereof to achieve a desired result. As shown, stressed layer 3103 is tensile 3107 or compressive 3109. Although the above has been described in terms of a single stressed layer, multiple stressed layers can be used. Alternatively, stressed layers can be combined with other layers. Additionally, a single material layer has been described. The single material layer can be replaced by multiple material layers and the like. Each of these layers can be homogeneous or graded or non-homogeneous or any combinations thereof. In the following discussion, the material layer is removed or cleaved from or within the stressed layer using a controlled cleaving action. Other ways of forming a stressed layer are described below.

FIGS. 12B to 12C are simplified diagrams of an alternative process for forming a stressed region, which is used to cleave a film of material from a substrate. These diagrams are merely examples, which should not limit the scope of the claims herein. One of ordinary skill in the art would recognize many other variations, alternatives, and modifications. Like reference numerals are used in these diagrams as others noted here, but are not intended to be limiting. Substrate 3010 is a silicon wafer which includes a material region 3012 to be removed, which is a thin relatively uniform film derived from the substrate material. The silicon wafer 3010 includes a top surface 3014, a bottom surface 3016, and a thickness 3018. Substrate 3010 also has a first side (side 1) and a second side (side 2). Material region 3012 also includes a thickness 3020, within the thickness 3018 of the silicon wafer. The present invention provides a novel technique for removing the material region 3012 using the following sequence of steps.

Selected energetic particles implant 3111 through the top surface 3014 of the silicon wafer to a region 3111A underlying a selected depth 3024, which defines the thickness 3020 of the material region 3012, termed the thin film of material. A variety of techniques can be used to implant the energetic particles into the silicon wafer. These techniques include ion implantation using, for example, beam line ion implantation equipment manufactured from companies such as Applied Materials, Eaton Corporation, Varian, and others. Alternatively, implantation occurs using a plasma immersion ion implantation (“PIII”) technique. Examples of plasma immersion implantation techniques are described in “Recent Applications of Plasma Immersion Ion Implantation,” Paul K. Chu, Chung Chan, and Nathan W. Cheung, SEMICONDUCTOR INTERNATIONAL, pp. 165-172, June 1996, and “Plasma Immersion Ion Implantation—A Fledgling Technique for Semiconductor Processing,”, P. K. Chu, S. Qin, C. Chan, N. W. Cheung, and L. A. Larson, MATERIAL SCIENCE AND ENGINEERING REPORTS, A Review Journal, pp. 207-280, Volume R17, Nos. 6-7, (Nov. 30, 1996), which are both hereby incorporated by reference for all purposes. Furthermore, implantation can occur using ion shower. Of course, techniques used depend upon the application.

Selected energetic particles 3113 particles implant 3111 through the top surface 3014 of the silicon wafer to a region 3113A overlying a selected depth 3024, which defines the thickness 3020 of the material region 3012, termed the thin film of material. A variety of techniques can be used to implant the energetic particles into the silicon wafer. These techniques include ion implantation using, for example, beam line ion implantation equipment manufactured from companies such as Applied Materials, Eaton Corporation, Varian, and others. Alternatively, implantation occurs using a plasma immersion ion implantation (“PIII”) technique. Examples of plasma immersion implantation techniques were noted. Furthermore, implantation can occur using ion shower. Of course, techniques used depend upon the application.

Depending upon the application, particles that increase a strength of the regions 3111A, 3113A. These particles can be almost any charged (e.g., positive or negative) and/or neutral atoms or molecules, or the like. In a specific embodiment, the particles can be neutral and/or charged particles including ions such as ions of nitrogen or oxygen. The particles can also be derived from compounds such as gases. Alternatively, the particles can be any combination of the above particles, and/or ions and/or molecular species and/or atomic species. The particles generally have sufficient kinetic energy to penetrate through the surface to the selected depth underneath the surface.

Effectively, the implanted particles add stress or reduce fracture energy along a plane parallel to the top surface of the substrate at the selected depth. The energies depend, in part, upon the implantation species and conditions. These particles reduce a fracture energy level of the substrate at the selected depth. This allows for a controlled cleave along the implanted plane at the selected depth. Implantation can occur under conditions such that the energy state of substrate at all internal locations is insufficient to initiate a non-reversible fracture (i.e., separation or cleaving) in the substrate material. It should be noted, however, that implantation does generally cause a certain amount of defects (e.g., micro-detects) in the substrate that can be repaired by subsequent heat treatment, e.g., thermal annealing or rapid thermal annealing. Overlying the silicon wafer is an oxide layer 2105. The oxide layer can be eliminated in some embodiments.

Once the stressed silicon wafer is made, the process uses a step of joining the silicon wafer to a workpiece or target wafer, as illustrated in FIG. 13. The workpiece may also be a variety of other types of substrates such as those made of a dielectric material (e.g., quartz, glass, silicon nitride, silicon dioxide), a conductive material (silicon, polysilicon, group III/V materials, metal), and plastics (e.g., polyimide-based materials). In the present example, however, the workpiece is a silicon wafer.

In a specific embodiment, the silicon wafers are joined or fused together using a low temperature thermal step. The low temperature thermal process generally ensures that the implanted particles do not place excessive stress on the material region, which can produce an uncontrolled cleave action. In one aspect, the low temperature bonding process occurs by a self-bonding process. In particular, one wafer (or both) is stripped to remove oxidation therefrom (or one wafer is not oxidized). A cleaning solution treats the surface of the wafer to form O—H bonds on the wafer surface. An example of a solution used to clean the wafer is a mixture of H₂O₂—H₂SO₄. A dryer dries the wafer surfaces to remove any residual liquids or particles from the wafer surfaces. Self-bonding occurs by placing a face of the cleaned wafer against the face of an oxidized wafer.

Alternatively, a self-bonding process occurs by activating one (or both) of the wafer surfaces to be bonded by plasma cleaning. In particular, plasma cleaning activates the wafer surface using a plasma derived from gases such as argon, ammonia, hydrogen, neon, water vapor, and oxygen. The activated wafer surface 2203 is placed against a face of the other wafer, which has a coat of oxidation 2205 thereon. The wafers are in a sandwiched structure having exposed wafer faces. A selected amount of pressure is placed on each exposed face of the wafers to self-bond one wafer to the other.

Alternatively, an adhesive disposed on the wafer surfaces is used to bond one wafer onto the other. The adhesive includes an epoxy, polyimide-type materials, and the like. Spin-on-glass layers can be used to bond one wafer surface onto the face of another. These spin-on-glass (“SOG”) materials include, among others, siloxanes or silicates, which are often mixed with alcohol-based solvents or the like. SOG can be a desirable material because of the low temperatures (e.g., 150 to 250° C.) often needed to cure the SOG after it is applied to surfaces of the wafers.

Alternatively, a variety of other low temperature techniques can be used to join the donor wafer to the target wafer. For instance, an electrostatic bonding technique can be used to join the two wafers together. In particular, one or both wafer surface(s) is charged to attract to the other wafer surface. Additionally, the donor wafer can be fused to the target wafer using a variety of commonly known techniques. Of course, the technique used depends upon the application.

After bonding the wafers into a sandwiched structure 2300, as shown in FIG. 14, the method includes a controlled cleaving action to remove the substrate material to provide a thin film of substrate material 2101 overlying an insulator 2305 the target silicon wafer 2201. The controlled-cleaving occurs by way of selective energy placement or positioning or targeting 2301, 2303 of energy sources onto the donor and/or target wafers. For instance, an energy impulse(s) can be used to initiate the cleaving action. The impulse (or impulses) is provided using an energy source which include, among others, a mechanical source, a chemical source, a thermal sink or source, and an electrical source.

The controlled cleaving action is initiated by way of any of the previously noted techniques and others and is illustrated by way of FIG. 14. For instance, a process for initiating the controlled cleaving action uses a step of providing energy 2301, 2303 to a selected region of the substrate to initiate a controlled cleaving action at the selected depth (z₀) in the substrate, whereupon the cleaving action is made using a propagating cleave front to free a portion of the substrate material to be removed from the substrate. In a specific embodiment, the method uses a single impulse to begin the cleaving action, as previously noted. Alternatively, the method uses an initiation impulse, which is followed by another impulse or successive impulses to selected regions of the substrate. Alternatively, the method provides an impulse to initiate a cleaving action which is sustained by a scanned energy along the substrate. Alternatively, energy can be scanned across selected regions of the substrate to initiate and/or sustain the controlled cleaving action.

Optionally, an energy or stress of the substrate material is increased toward an energy level necessary to initiate the cleaving action, but not enough to initiate the cleaving action before directing an impulse or multiple successive impulses to the substrate according to the present invention. The global energy state of the substrate can be raised or lowered using a variety of sources such as chemical, mechanical, thermal (sink or source), or electrical, alone or in combination. The chemical source can include particles, fluids, gases, or liquids. These sources can also include chemical reaction to increase stress in the material region. The chemical source is introduced as flood, time-varying, spatially varying, or continuous. In other embodiments, a mechanical source is derived from rotational, translational, compressional, expansional, or ultrasonic energies. The mechanical source can be introduced as flood, time-varying, spatially varying, or continuous. In further embodiments, the electrical source is selected from an applied voltage or an applied electro-magnetic field, which is introduced as flood, time-varying, spatially varying, or continuous. In still further embodiments, the thermal source or sink is selected from radiation, convection, or conduction. This thermal source can be selected from, among others, a photon beam, a fluid jet, a liquid jet, a gas jet, an electro/magnetic field, an electron beam, a thermo-electric heating, and a furnace. The thermal sink can be selected from a fluid jet, a liquid jet, a gas jet, a cryogenic fluid, a super-cooled liquid, a thermoelectric cooling means, an electro/magnetic field, and others. Similar to the previous embodiments, the thermal source is applied as flood, time-varying, spatially varying, or continuous. Still further, any of the above embodiments can be combined or even separated, depending upon the application. Of course, the type of source used depends upon the application. As noted, the global source increases a level of energy or stress in the material region without initiating a cleaving action in the material region before providing energy to initiate the controlled cleaving action.

In a preferred embodiment, the method maintains a temperature which is below a temperature of introducing the particles into the substrate. In some embodiments, the substrate temperature is maintained between −200 and 450° C. during the step of introducing energy to initiate propagation of the cleaving action. Substrate temperature can also be maintained at a temperature below 400° C. or below 350° C. In preferred embodiments, the method uses a thermal sink to initiate and maintain the cleaving action, which occurs at conditions significantly below room temperature.

In an alternative preferred embodiment, the mechanical and/or thermal source can be a fluid jet that is pressurized (e.g., compressional) according to an embodiment of the present invention. The fluid jet (or liquid jet or gas jet) impinges on an edge region of substrate 2300 to initiate the controlled cleaving process. The fluid jet from a compressed or pressurized fluid source is directed to a region at the selected depth 2111 to cleave a thickness of material region 2101 from substrate 2100. The fluid jet separates region 2101 from substrate 2100 that separate from each other at selected depth 2111. The fluid jet can be adjusted to initiate and maintain the controlled cleaving process to separate material 2101 from substrate 2100. Depending upon the application, the fluid jet can be adjusted in direction, location, and magnitude to achieve the desired controlled cleaving process.

A final bonding step occurs between the target wafer and thin film of material region according to some embodiments, as illustrated by FIG. 15. In one embodiment, one silicon wafer has an overlying layer of silicon dioxide, which is thermally grown overlying the face before cleaning the thin film of material. The silicon dioxide can also be formed using a variety of other techniques, e.g., chemical vapor deposition. The silicon dioxide between the wafer surfaces fuses together thermally in this process.

In some embodiments, the oxidized silicon surface from either the target wafer or the thin film of material region (from the donor wafer) are further pressed together and are subjected to an oxidizing ambient 2401. The oxidizing ambient can be in a diffusion furnace for steam oxidation, hydrogen oxidation, or the like. A combination of the pressure and the oxidizing ambient fuses the two silicon wafers together at the oxide surface or interface 2305. These embodiments often require high temperatures (e.g., 700° C.).

Alternatively, the two silicon surfaces are further pressed together and subjected to an applied voltage between the two wafers. The applied voltage raises temperature of the wafers to induce a bonding between the wafers. This technique limits the amount of crystal defects introduced into the silicon wafers during the bonding process, since substantially no mechanical force is needed to initiate the bonding action between the wafers. Of course, the technique used depends upon the application.

After bonding the wafers, silicon-on-insulator has a target substrate with an overlying film of silicon material and a sandwiched oxide layer between the target substrate and the silicon film, as also illustrated in FIG. 15. The detached surface of the film of silicon material is often rough 2404 and needs finishing. Finishing occurs using a combination of grinding and/or polishing techniques. In some embodiments, the detached surface undergoes a step of grinding using, for examples, techniques such as rotating an abrasive material overlying the detached surface to remove any imperfections or surface roughness therefrom. A machine such as a “back grinder” made by a company called Disco may provide this technique. Alternatively, a smoothing operation may be carried out using a combination of hydrogen treatment and chemical reaction in an epi-reactor, for example.

Alternatively, chemical mechanical polishing or planarization (“CMP”) techniques finish the detached surface of the film, as illustrated by FIG. 16. In CMP, a slurry mixture is applied directly to a polishing surface 2501 which is attached to a rotating platen 2503. This slurry mixture can be transferred to the polishing surface by way of an orifice, which is coupled to a slurry source. The slurry is often a solution containing an abrasive and an oxidizer, e.g., H₂O₂, KIO₃, ferric nitrate. The abrasive is often a borosilicate glass, titanium dioxide, titanium nitride, aluminum oxide, aluminum trioxide, iron nitrate, cerium oxide, silicon dioxide (colloidal silica), silicon nitride, silicon carbide, graphite, diamond, and any mixtures thereof. This abrasive is mixed in a solution of deionized water and oxidizer or the like. Preferably, the solution is acidic.

This acid solution generally interacts with the silicon material from the wafer during the polishing process. The polishing process preferably uses a poly-urethane polishing pad. An example of this polishing pad is one made by Rodel and sold under the tradename of IC-1000. The polishing pad is rotated at a selected speed. A carrier head which picks up the target wafer having the film applies a selected amount of pressure on the backside of the target wafer such that a selected force is applied to the film. The polishing process removes about a selected amount of film material, which provides a relatively smooth film surface 2601 for subsequent processing, as illustrated by FIG. 17.

In certain embodiments, a thin film of oxide 2406 overlies the film of material overlying the target wafer, as illustrated in FIG. 15. The oxide layer forms during the thermal annealing step, which is described above for permanently bonding the film of material to the target wafer. In these embodiments, the finishing process is selectively adjusted to first remove oxide and the film is subsequently polished to complete the process. Of course, the sequence of steps depends upon the particular application.

In a specific embodiment, the silicon-on-insulator substrate undergoes a series of process steps for formation of integrated circuits thereon. These processing steps are described in S. Wolf, Silicon Processing for the VLSI Era (Volume 2), Lattice Press (1990), which is hereby incorporated by reference for all purposes. A portion of a completed wafer 2700 including integrated circuit devices is illustrated by FIG. 18. As shown, the portion of the wafer 2700 includes active devices regions 2701 and isolation regions 2703. The active devices are field effect transistors each having a source/drain region 2705 and a gate electrode 2707. A dielectric isolation layer 2709 is defined overlying the active devices to isolate the active devices from any overlying layers.

Although the above description is in terms of a silicon wafer, other substrates may also be used. For example, the substrate can be almost any monocrystalline, polycrystalline, or even amorphous type substrate. Additionally, the substrate can be made of III/V materials such as gallium arsenide, gallium nitride (GaN), and others. The multi-layered substrate can also be used according to the present invention. The multi-layered substrate includes a silicon-on-insulator substrate, a variety of sandwiched layers on a semiconductor substrate, and numerous other types of substrates. Additionally, the embodiments above were generally in terms of providing a pulse of energy to initiate a controlled cleaving action. The pulse can be replaced by energy that is scanned across a selected region of the substrate to initiate the controlled cleaving action. Energy can also be scanned across selected regions of the substrate to sustain or maintain the controlled cleaving action. One of ordinary skill in the art would easily recognize a variety of alternatives, modifications, and variations, which can be used according to the present invention.

While the above is a full description of the specific embodiments, various modifications, alternative constructions and equivalents may be used. Therefore, the above description and illustrations should not be taken as limiting the scope of the present invention which is defined by the appended claims. 

What is claimed is:
 1. A process for forming a film of material from substrates, said process comprising: forming a stressed region at a selected depth underneath a surface of a substrate, said stressed region at said selected depth to define a substrate material to be removed above said selected depth; and providing energy using a fluid to a selected region of said substrate to initiate a controlled cleaving action at said selected depth in said substrate, whereupon said cleaving action is made using a propagating cleave front to free a portion of said material to be removed from said substrate.
 2. The process of claim 1 wherein said stressed region is derived from a layer formed from chemical vapor deposition.
 3. The process of claim 1 wherein said stressed region is derived from layer formed by physical vapor deposition.
 4. The process of claim 1 wherein said providing energy sustains said controlled cleaving action to remove said material from said substrate to provide a film of material.
 5. The process of claim 1 wherein said providing energy increases a controlled stress in said material and sustains said controlled cleaving action to remove said material from said substrate to provide a film of material.
 6. The process of claim 1 further comprising providing additional energy to said substrate to sustain said controlled cleaving action to remove said material from said substrate to provide a film of material.
 7. The process of claim 1 further comprising providing additional energy to said substrate to increases a controlled stress in said material and sustains said controlled cleaving action to remove said material from said substrate to provide a film of material.
 8. The process of claim 1 wherein said forming step comprises forming a stressed layer overlying a donor substrate and forming the material layer to be removed overlying the stressed layer.
 9. The process of claim 1 wherein said propagating cleave front is selected from a single cleave front or multiple cleave fronts.
 10. The process of claim 1 wherein said substrate is made of a material selected from the group consisting of silicon, diamond, quartz, glass, sapphire, silicon carbide, dielectric, group III/V material, plastic, ceramic material, and multi-layered substrate.
 11. The process of claim 1 wherein said surface is planar.
 12. The process of claim 1 wherein said surface is curved.
 13. The process of claim 1 wherein said substrate is a silicon substrate comprising an overlying layer of dielectric material, said selected depth being underneath said dielectric material.
 14. The process of claim 1 wherein said fluid is selected from a static source or a fluid jet source.
 15. The process of claim 1 wherein said fluid is directed to said selected depth to initiate said controlled cleaving action.
 16. The process of claim 1 wherein said fluid is derived from a compressed gas.
 17. A process for forming a multilayered substrate, said process comprising. providing a multilayered substrate, said substrate comprising a substrate portion having a stressed region at a selected depth to define a substrate material to be removed above said selected depth; and providing a fluid to a selected region of said substrate to initiate a controlled cleaving action at said selected depth in said substrate, whereupon said cleaving action is made using a propagating cleave front to free a portion of said material to be removed from said substrate.
 18. The process of claim 17 wherein said fluid is selected from a static source or a fluid jet source.
 19. The process of claim 17 wherein said fluid jet is directed to said selected depth to initiate said controlled cleaving action.
 20. The process of claim 17 wherein said fluid jet is derived from a compressed gas.
 21. A process for forming a film of material from substrates, said process comprising: providing a bulk substrate comprising an upper surface; forming a first compressive layer overlying the upper surface; forming a tensile layer overlying the first compressive layer; forming a second compressive layer overlying the tensile layer; forming a material layer overlying the second compressive layer; and providing energy to a selected region of the tensile layer to initiate a controlled cleaving action at the tensile layer, whereupon the cleaving action is made using a propagating cleave front to free the material layer from the bulk substrate.
 22. The process of claim 21 wherein the tensile layer comprises a silicon-germanium-carbon alloy.
 23. The process of claim 21 wherein the first compressive layer comprises a silicon-germanium alloy.
 24. The process of claim 21 wherein the energy is provided by a fluid directed to the selected region.
 25. The process of claim 22 wherein the second compressive layer comprises a silicon germanium alloy.
 26. A process for forming a film of material from substrates, said process comprising: providing a bulk substrate comprising an upper surface; forming a cleaving layer overlying the upper surface; forming a material layer overlying the cleaving layer; and providing energy to a selected region of the cleaving layer to initiate a controlled cleaving action at the cleaving layer, whereupon the cleaving action is made using a propagating cleave front to free the material layer from the bulk substrate.
 27. The process of claim 26 wherein the energy is provided using a pressurized fluid at the selected region. 